DE1578081B2 - Duesenrohrausbildung zur steuerung eines flugkoerpers - Google Patents

Duesenrohrausbildung zur steuerung eines flugkoerpers

Info

Publication number
DE1578081B2
DE1578081B2 DE1967B0091700 DEB0091700A DE1578081B2 DE 1578081 B2 DE1578081 B2 DE 1578081B2 DE 1967B0091700 DE1967B0091700 DE 1967B0091700 DE B0091700 A DEB0091700 A DE B0091700A DE 1578081 B2 DE1578081 B2 DE 1578081B2
Authority
DE
Germany
Prior art keywords
nozzle tube
control
nozzle
opposite
missile
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
DE1967B0091700
Other languages
German (de)
English (en)
Other versions
DE1578081A1 (de
Inventor
Cyrille Francois VaI d'Albian par Jouy-en-Josas; Oudin Francois Noisy-le-Roi; Pavlin (Frankreich)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bertin Technologies SAS
Original Assignee
Bertin et Cie SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bertin et Cie SA filed Critical Bertin et Cie SA
Publication of DE1578081A1 publication Critical patent/DE1578081A1/de
Publication of DE1578081B2 publication Critical patent/DE1578081B2/de
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
DE1967B0091700 1966-03-22 1967-03-21 Duesenrohrausbildung zur steuerung eines flugkoerpers Granted DE1578081B2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR54510A FR1488272A (fr) 1966-03-22 1966-03-22 Système de pilotage de missiles

Publications (2)

Publication Number Publication Date
DE1578081A1 DE1578081A1 (de) 1971-09-16
DE1578081B2 true DE1578081B2 (de) 1976-07-22

Family

ID=8604395

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1967B0091700 Granted DE1578081B2 (de) 1966-03-22 1967-03-21 Duesenrohrausbildung zur steuerung eines flugkoerpers

Country Status (5)

Country Link
US (1) US3502288A (cs)
BE (1) BE695600A (cs)
DE (1) DE1578081B2 (cs)
FR (1) FR1488272A (cs)
GB (1) GB1185193A (cs)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3711013A (en) * 1971-04-26 1973-01-16 Rohr Corp Thrust control and sound apparatus
US3739984A (en) * 1971-08-25 1973-06-19 Rohr Industries Inc Thrust augmenting and south suppressing apparatus and method
DE2846372C2 (de) * 1978-10-25 1985-11-21 Rheinmetall GmbH, 4000 Düsseldorf Geschoß mit radialgerichteten Steuerdüsen zur Endphasenlenkung
US4384690A (en) * 1981-03-06 1983-05-24 The United States Of America As Represented By The Secretary Of The Navy Thrust vector control for large deflection angles
EP0245565B1 (fr) * 1986-05-12 1991-03-13 AEROSPATIALE Société Nationale Industrielle Procédé de pilotage d'un missile à faible vitesse, système d'arme et missile pour la mise en oeuvre du procédé
FR2578665B1 (fr) * 1981-06-04 1988-02-12 Aerospatiale Procede de pilotage d'un missile a faible vitesse, systeme d'arme et missile pour la mise en oeuvre du procede
FR2536720A1 (fr) * 1982-11-29 1984-06-01 Aerospatiale Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux et missile comportant un tel systeme
JPH0830640B2 (ja) * 1986-05-22 1996-03-27 アエロスパテイアル・ソシエテ・ナシヨナル・アンダストリエル ミサイル
US5273237A (en) * 1992-11-02 1993-12-28 The United States Of America As Represented By The Secretary Of The Air Force Forebody nozzle for aircraft directional control
US8186145B2 (en) * 2008-02-26 2012-05-29 Aerojet-General Corporation Rocket nozzles for unconventional vehicles
US9018572B2 (en) * 2012-11-06 2015-04-28 Raytheon Company Rocket propelled payload with divert control system within nose cone
RU2558502C1 (ru) * 2014-05-13 2015-08-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Поволжский государственный технологический университет" Способ управления ракетой
WO2022023790A1 (en) * 2020-07-28 2022-02-03 Eijadi Ramin Conceptual design of a modern multi-purpose actuator with the capability of performance similar to control surfaces

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2694898A (en) * 1948-08-09 1954-11-23 France Etat Device for deflecting a high-speed jet of gas ejected through a nozzle
US2726510A (en) * 1952-03-26 1955-12-13 Daniel And Florence Guggenhcim Flight-control apparatus involving steering combustion chambers
US3016066A (en) * 1960-01-22 1962-01-09 Raymond W Warren Fluid oscillator
US3158166A (en) * 1962-08-07 1964-11-24 Raymond W Warren Negative feedback oscillator
US3246863A (en) * 1962-10-25 1966-04-19 Honeywell Inc Control apparatus
US3279185A (en) * 1963-07-18 1966-10-18 George D Lewis Rocket steering system
US3228410A (en) * 1963-09-30 1966-01-11 Raymond W Warren Fluid pulse width modulation
US3325103A (en) * 1964-08-05 1967-06-13 Aerospace Corp Thrust vector control for reaction engines

Also Published As

Publication number Publication date
BE695600A (cs) 1967-09-18
DE1578081A1 (de) 1971-09-16
FR1488272A (fr) 1967-07-13
GB1185193A (en) 1970-03-25
US3502288A (en) 1970-03-24

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
E77 Valid patent as to the heymanns-index 1977
EHJ Ceased/non-payment of the annual fee